Patents
Patents for F01D 11 - Preventing or minimising internal leakage of working fluid, e.g. between stages (10,581)
03/2015
03/05/2015WO2015031764A1 Blade outer air seal made of ceramic matrix composite
03/05/2015WO2015031763A1 Seal for gas turbine engine
03/05/2015WO2015031384A1 Bifurcated sliding seal
03/05/2015WO2015030946A1 Gas turbine engine with fan clearance control
03/05/2015WO2015028177A1 Brush seal arrangement
03/05/2015US20150064012 Blade of a rotary flow machine with a radial strip seal
03/05/2015US20150064008 Turbomachine bucket having angel wing for differently sized discouragers and related methods
03/05/2015US20150063990 Turbomachine Axial Compressor Seal with a Brush Seal
03/05/2015US20150063981 Device for sealing between the coaxial shafts of a turbomachine
03/05/2015US20150061228 Sealing arrangement in an axial turbomachine
03/05/2015DE112013002248T5 Aktuatorstangen-Dichtsystem Actuator rods sealing system
03/05/2015DE102013217581A1 Dichtungsanordnung in einer axialen Strömungsmaschine Seal assembly in an axial flow machine
03/04/2015EP2843198A1 Method and control system for active rotor tip control clearance
03/04/2015EP2843197A2 Blade of a rotary flow machine with a radial strip seal
03/04/2015EP2843196A1 Compressor of an axial turbomachine with brush seal and corresponding turbomachine
03/03/2015US8970228 Rotational clearance measurement system and method of operation
03/03/2015US8967974 Composite airfoil assembly
03/03/2015US8967973 Turbine bucket platform shaping for gas temperature control and related method
03/03/2015US8967957 Rotating airfoil component of a turbomachine
03/03/2015US8967955 Turbocharger with variable nozzle having labyrinth seal for vanes
03/03/2015US8967627 Intershaft seal
02/2015
02/26/2015WO2015026534A1 Belly band seal with circumferential spacer
02/26/2015US20150056068 Belly band seal with circumferential spacer
02/26/2015US20150054362 Method and Device for Sensorless Control of a Separately Excited Synchronous Machine
02/26/2015DE112013001882T5 Axialturbine mit Sicherheitsummantelung Axial turbine with protective enclosure
02/26/2015DE102013210876B4 Verbundbauteil zur thermischen Spaltsteuerung in einer Strömungsmaschine sowie dieses enthaltende Strömungsmaschine Composite component for thermal gap control in a turbomachine, and this flow containing machine
02/25/2015EP2840229A1 Flow guide within a steam turbine seal
02/25/2015EP2839117A1 Turbine stage for a turbomachine
02/24/2015US8961151 Turbocharger
02/24/2015US8961137 Turbine wheel for a turbine engine
02/24/2015US8961135 Mateface gap configuration for gas turbine engine
02/24/2015US8961132 Secondary flow arrangement for slotted rotor
02/24/2015US8961117 Insulating a circumferential rim of an outer casing of a turbine engine from a corresponding ring sector
02/24/2015US8961115 Clearance control for gas turbine engine seal
02/24/2015CA2598259C Simple axial retention feature for abradable members
02/19/2015WO2015023471A1 Flow vortex spoiler
02/19/2015WO2015023321A2 Radial position control of case supported structure with axial reaction member
02/19/2015US20150050151 Annulus filler
02/19/2015US20150050150 Annulus filler
02/19/2015US20150050138 Fixation device for turbine and method for applying fixation
02/19/2015US20150050130 Sealing device between two axisymmetric coaxial parts
02/19/2015US20150050127 Air with integral spring for a gas turbine engine exhaust drive
02/19/2015US20150050125 Fluid seal arrangement and method for constricting a leakage flow through a leakage gap
02/19/2015US20150048618 Turbine generator
02/19/2015US20150047356 Turbine engine, such as a turbojet or a turboprop engine
02/19/2015DE102013216400A1 Leitschaufel mit einer Borsten umfassenden Dichteinrichtung Vane with a comprehensive bristles sealing device
02/18/2015EP2837860A1 Brush seal
02/18/2015EP2837858A1 Brush seal
02/18/2015EP2837774A1 Annulus filler and corresponding stage and gas turbine engine
02/18/2015EP2837773A1 Annulus filler and corresponding stage and gas turbine engine
02/18/2015EP2837772A1 Annulus filler and corresponding stage and gas turbine engine
02/18/2015EP2836684A1 Turbine engine, such as a turbojet or a turboprop engine
02/17/2015US8956120 Non-continuous ring seal
02/17/2015US8956106 Adaptive eductor system
02/17/2015US8956104 Bucket assembly for turbine system
02/12/2015WO2015021247A1 High porosity abradable coating
02/12/2015WO2015021222A1 Clearance control assembly
02/12/2015WO2015021029A1 Boas with radial load feature
02/12/2015WO2015020775A1 Gas turbine engine aft seal plate geometry
02/12/2015WO2015020708A2 Gas turbine rapid response clearance control system with annular piston
02/12/2015WO2015018841A1 Insert element, ring segment, gas turbine, mounting method
02/12/2015WO2015018839A1 Insert element, ring segment, gas turbine, and assembly method
02/12/2015US20150044035 High porosity abradable coating
02/12/2015US20150044018 Active seal system
02/12/2015US20150040567 Systems and Methods for Reducing or Limiting One or More Flows Between a Hot Gas Path and a Wheel Space of a Turbine
02/12/2015US20150040566 Helical seal system for a turbomachine
02/12/2015DE102014111201A1 Systeme und Verfahren zur Reduktion oder Beschränkung einer oder mehrerer Strömungen zwischen einem Heißgaspfad und dem Rotorinnenraum einer Turbine Systems and methods for the reduction or limitation of one or more flows between a hot gas path and the rotor interior of a turbine
02/12/2015DE10140742B4 Vorrichtung zur Dichtspaltreduzierung zwischen einer rotierenden und einer stationären Komponente innerhalb einer axial durchströmten Strömungsmaschine A device for sealing gap reduction between a rotating and a stationary component in an axial-flow turbomachine
02/11/2015EP2835504A1 Insert element and gas turbine
02/11/2015EP2835502A2 Blade of a turbine
02/11/2015EP2835500A1 Insert element and gas turbine
02/11/2015EP2834502A1 Axial non-contact seal
02/11/2015CN104350238A 覆盖有耐磨涂层的涡轮机定子壁 Covered with a wear-resistant coating of turbine stator wall
02/11/2015CN104343473A 一种用于有机工质向心透平的轴端密封装置 A shaft sealing device to the heart of the organic working fluids for turbine
02/11/2015CN104343472A 具有改进的密封的涡轮叶片和涡轮 Having improved sealing of the turbine blades and turbine
02/10/2015US8951014 Turbine blade with mate face cooling air flow
02/10/2015US8951008 Compressor blade and production and use of a compressor blade
02/10/2015US8950751 Compliant element
02/05/2015WO2015017040A2 Gas turbine engine vane ring arrangement
02/05/2015US20150037145 Systems relating to axial positioning turbine casings and blade tip clearance in gas turbine engines
02/05/2015US20150037142 Casing for turbomachine blish and turbomachine equipped with said casing
02/05/2015US20150037133 System and method relating to axial positioning turbine casings and blade tip clearance in gas turbine engines
02/05/2015DE102014110749A1 Systeme und Verfahren betreffend die axiale Positionierung von Turbinengehäusen und den Schaufelspitzenspalt in Gasturbinen Systems and procedures concerning the axial positioning of turbine housings and the blade tip clearance in gas turbines
02/04/2015EP2832975A1 Seal member, turbine, and gas turbine
02/04/2015EP2832952A1 Turbine blade and turbine with improved sealing
02/04/2015EP2831380A1 Knife edge seal for gas turbine engine
02/04/2015EP2831376A1 Turbine blade
02/04/2015CN204140141U 主动控制叶尖间隙的执行机构和系统 Active tip clearance control actuators and systems
02/04/2015CN204140140U 一种用于燃气轮机封严的止扣环结构 Only grommet seal structure for a gas turbine of
02/04/2015CN104329125A 燃气轮机 Gas turbine
02/03/2015US8944762 Spoked spacer for a gas turbine engine
02/03/2015US8944756 Blade outer air seal assembly
02/03/2015US8944751 Turbine nozzle cooling assembly
01/2015
01/29/2015WO2015013503A1 Trough seal for gas turbine engine
01/29/2015WO2015013114A1 Turbocharger purge seal including axisymmetric supply cavity
01/29/2015WO2015010740A1 Sealing arrangement for a turbomachine
01/29/2015US20150030826 Method for creating a textured bond coat surface
01/29/2015US20150030442 Seal member, turbine, and gas turbine
01/29/2015US20150030433 Method and apparatus for measuring turbine shell clearance
01/28/2015EP2829689A1 Insulating structure for a thermal gas turbine, coresponding thermal gas turbine and method of manufacturing
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